A 9700-hour durability test of a five centimeter diameter ion thruster
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1973-1111
Reference8 articles.
1. W munications Satellites," Paper 72-1150, Nov. 1972, AIAAISAE. New Orleans, La.
2. An 8-cm electron bombardment thruster for auxiliary propulsion
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1. Development of an 8-cm engineering model thruster system;12th International Electric Propulsion Conference;1976-08-16
2. Hollow cathode characteristics in high current discharges;11th Electric Propulsion Conference;1975-03-19
3. 8-cm mercury ion thruster system technology;10th Propulsion Conference;1974-08-16
4. Ion propulsion flight experience life tests and reliability estimates;9th Propulsion Conference;1973-08-16
5. Current technology in ion and electrothermal propulsion;9th Propulsion Conference;1973-08-16
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